mirror of
https://github.com/PX4/PX4-Autopilot.git
synced 2026-05-25 16:56:25 +08:00
Merge remote-tracking branch 'upstream/master' into hkmicropcb
This commit is contained in:
@@ -20,7 +20,7 @@ then
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param set MC_PITCHRATE_D 0.0025
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param set MC_YAW_P 2.8
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param set MC_YAWRATE_P 0.28
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param set MC_YAWRATE_I 0.0
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param set MC_YAWRATE_I 0.1
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param set MC_YAWRATE_D 0.0
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fi
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@@ -19,7 +19,7 @@ then
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param set MC_PITCHRATE_D 0.003
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param set MC_YAW_P 2.8
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param set MC_YAWRATE_P 0.2
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param set MC_YAWRATE_I 0.0
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param set MC_YAWRATE_I 0.1
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param set MC_YAWRATE_D 0.0
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fi
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@@ -20,7 +20,7 @@ then
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param set MC_PITCHRATE_D 0.003
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param set MC_YAW_P 2.8
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param set MC_YAWRATE_P 0.2
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param set MC_YAWRATE_I 0.0
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param set MC_YAWRATE_I 0.1
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param set MC_YAWRATE_D 0.0
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fi
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@@ -14,7 +14,7 @@ then
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param set MC_PITCHRATE_D 0.003
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param set MC_YAW_P 2.8
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param set MC_YAWRATE_P 0.2
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param set MC_YAWRATE_I 0.0
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param set MC_YAWRATE_I 0.1
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param set MC_YAWRATE_D 0.0
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param set MC_YAW_FF 0.5
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@@ -132,6 +132,10 @@ then
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#
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if param compare SYS_AUTOCONFIG 1
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then
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# We can't be sure the defaults haven't changed, so
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# if someone requests a re-configuration, we do it
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# cleanly from scratch (except autostart / autoconfig)
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param reset_nostart
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set DO_AUTOCONFIG yes
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else
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set DO_AUTOCONFIG no
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@@ -0,0 +1,2 @@
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#!/bin/sh
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python px_process_params.py --xml
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@@ -559,13 +559,7 @@ BlinkM::led()
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}
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/* get number of used satellites in navigation */
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num_of_used_sats = 0;
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for(unsigned satloop=0; satloop<sizeof(vehicle_gps_position_raw.satellite_used); satloop++) {
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if(vehicle_gps_position_raw.satellite_used[satloop] == 1) {
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num_of_used_sats++;
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}
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}
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num_of_used_sats = vehicle_gps_position_raw.satellites_used;
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if (new_data_vehicle_status || no_data_vehicle_status < 3) {
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if (num_of_cells == 0) {
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+91
-48
@@ -63,6 +63,7 @@
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#include <drivers/drv_gps.h>
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#include <uORB/uORB.h>
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#include <uORB/topics/vehicle_gps_position.h>
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#include <uORB/topics/satellite_info.h>
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#include <board_config.h>
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@@ -79,10 +80,18 @@
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#endif
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static const int ERROR = -1;
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/* class for dynamic allocation of satellite info data */
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class GPS_Sat_Info
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{
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public:
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struct satellite_info_s _data;
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};
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class GPS : public device::CDev
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{
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public:
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GPS(const char *uart_path, bool fake_gps);
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GPS(const char *uart_path, bool fake_gps, bool enable_sat_info);
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virtual ~GPS();
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virtual int init();
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@@ -100,14 +109,17 @@ private:
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int _serial_fd; ///< serial interface to GPS
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unsigned _baudrate; ///< current baudrate
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char _port[20]; ///< device / serial port path
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volatile int _task; //< worker task
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volatile int _task; ///< worker task
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bool _healthy; ///< flag to signal if the GPS is ok
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bool _baudrate_changed; ///< flag to signal that the baudrate with the GPS has changed
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bool _baudrate_changed; ///< flag to signal that the baudrate with the GPS has changed
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bool _mode_changed; ///< flag that the GPS mode has changed
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gps_driver_mode_t _mode; ///< current mode
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GPS_Helper *_Helper; ///< instance of GPS parser
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struct vehicle_gps_position_s _report; ///< uORB topic for gps position
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orb_advert_t _report_pub; ///< uORB pub for gps position
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GPS_Sat_Info *_Sat_Info; ///< instance of GPS sat info data object
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struct vehicle_gps_position_s _report_gps_pos; ///< uORB topic for gps position
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orb_advert_t _report_gps_pos_pub; ///< uORB pub for gps position
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struct satellite_info_s *_p_report_sat_info; ///< pointer to uORB topic for satellite info
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orb_advert_t _report_sat_info_pub; ///< uORB pub for satellite info
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float _rate; ///< position update rate
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bool _fake_gps; ///< fake gps output
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@@ -154,14 +166,17 @@ GPS *g_dev;
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}
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GPS::GPS(const char *uart_path, bool fake_gps) :
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GPS::GPS(const char *uart_path, bool fake_gps, bool enable_sat_info) :
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CDev("gps", GPS_DEVICE_PATH),
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_task_should_exit(false),
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_healthy(false),
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_mode_changed(false),
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_mode(GPS_DRIVER_MODE_UBX),
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_Helper(nullptr),
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_report_pub(-1),
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_Sat_Info(nullptr),
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_report_gps_pos_pub(-1),
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_p_report_sat_info(nullptr),
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_report_sat_info_pub(-1),
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_rate(0.0f),
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_fake_gps(fake_gps)
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{
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@@ -172,7 +187,14 @@ GPS::GPS(const char *uart_path, bool fake_gps) :
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/* we need this potentially before it could be set in task_main */
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g_dev = this;
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memset(&_report, 0, sizeof(_report));
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memset(&_report_gps_pos, 0, sizeof(_report_gps_pos));
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/* create satellite info data object if requested */
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if (enable_sat_info) {
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_Sat_Info = new(GPS_Sat_Info);
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_p_report_sat_info = &_Sat_Info->_data;
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memset(_p_report_sat_info, 0, sizeof(*_p_report_sat_info));
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}
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_debug_enabled = true;
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}
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@@ -207,7 +229,7 @@ GPS::init()
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/* start the GPS driver worker task */
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_task = task_spawn_cmd("gps", SCHED_DEFAULT,
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SCHED_PRIORITY_SLOW_DRIVER, 2000, (main_t)&GPS::task_main_trampoline, nullptr);
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SCHED_PRIORITY_SLOW_DRIVER, 1500, (main_t)&GPS::task_main_trampoline, nullptr);
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if (_task < 0) {
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warnx("task start failed: %d", errno);
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@@ -271,33 +293,33 @@ GPS::task_main()
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if (_fake_gps) {
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_report.timestamp_position = hrt_absolute_time();
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_report.lat = (int32_t)47.378301e7f;
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_report.lon = (int32_t)8.538777e7f;
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_report.alt = (int32_t)1200e3f;
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_report.timestamp_variance = hrt_absolute_time();
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_report.s_variance_m_s = 10.0f;
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_report.p_variance_m = 10.0f;
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_report.c_variance_rad = 0.1f;
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_report.fix_type = 3;
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_report.eph = 0.9f;
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_report.epv = 1.8f;
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_report.timestamp_velocity = hrt_absolute_time();
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_report.vel_n_m_s = 0.0f;
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_report.vel_e_m_s = 0.0f;
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_report.vel_d_m_s = 0.0f;
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_report.vel_m_s = sqrtf(_report.vel_n_m_s * _report.vel_n_m_s + _report.vel_e_m_s * _report.vel_e_m_s + _report.vel_d_m_s * _report.vel_d_m_s);
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_report.cog_rad = 0.0f;
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_report.vel_ned_valid = true;
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_report_gps_pos.timestamp_position = hrt_absolute_time();
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_report_gps_pos.lat = (int32_t)47.378301e7f;
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_report_gps_pos.lon = (int32_t)8.538777e7f;
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_report_gps_pos.alt = (int32_t)1200e3f;
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_report_gps_pos.timestamp_variance = hrt_absolute_time();
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_report_gps_pos.s_variance_m_s = 10.0f;
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_report_gps_pos.p_variance_m = 10.0f;
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_report_gps_pos.c_variance_rad = 0.1f;
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_report_gps_pos.fix_type = 3;
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_report_gps_pos.eph = 0.9f;
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_report_gps_pos.epv = 1.8f;
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_report_gps_pos.timestamp_velocity = hrt_absolute_time();
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_report_gps_pos.vel_n_m_s = 0.0f;
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_report_gps_pos.vel_e_m_s = 0.0f;
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_report_gps_pos.vel_d_m_s = 0.0f;
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_report_gps_pos.vel_m_s = sqrtf(_report_gps_pos.vel_n_m_s * _report_gps_pos.vel_n_m_s + _report_gps_pos.vel_e_m_s * _report_gps_pos.vel_e_m_s + _report_gps_pos.vel_d_m_s * _report_gps_pos.vel_d_m_s);
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_report_gps_pos.cog_rad = 0.0f;
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_report_gps_pos.vel_ned_valid = true;
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//no time and satellite information simulated
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if (!(_pub_blocked)) {
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if (_report_pub > 0) {
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orb_publish(ORB_ID(vehicle_gps_position), _report_pub, &_report);
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if (_report_gps_pos_pub > 0) {
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orb_publish(ORB_ID(vehicle_gps_position), _report_gps_pos_pub, &_report_gps_pos);
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} else {
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_report_pub = orb_advertise(ORB_ID(vehicle_gps_position), &_report);
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_report_gps_pos_pub = orb_advertise(ORB_ID(vehicle_gps_position), &_report_gps_pos);
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}
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}
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@@ -313,11 +335,11 @@ GPS::task_main()
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switch (_mode) {
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case GPS_DRIVER_MODE_UBX:
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_Helper = new UBX(_serial_fd, &_report);
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_Helper = new UBX(_serial_fd, &_report_gps_pos, _p_report_sat_info);
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break;
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|
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case GPS_DRIVER_MODE_MTK:
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_Helper = new MTK(_serial_fd, &_report);
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_Helper = new MTK(_serial_fd, &_report_gps_pos);
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break;
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|
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default:
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@@ -332,20 +354,33 @@ GPS::task_main()
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// GPS is obviously detected successfully, reset statistics
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_Helper->reset_update_rates();
|
||||
|
||||
while (_Helper->receive(TIMEOUT_5HZ) > 0 && !_task_should_exit) {
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int helper_ret;
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while ((helper_ret = _Helper->receive(TIMEOUT_5HZ)) > 0 && !_task_should_exit) {
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// lock();
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/* opportunistic publishing - else invalid data would end up on the bus */
|
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|
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if (!(_pub_blocked)) {
|
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if (_report_pub > 0) {
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orb_publish(ORB_ID(vehicle_gps_position), _report_pub, &_report);
|
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if (helper_ret & 1) {
|
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if (_report_gps_pos_pub > 0) {
|
||||
orb_publish(ORB_ID(vehicle_gps_position), _report_gps_pos_pub, &_report_gps_pos);
|
||||
|
||||
} else {
|
||||
_report_pub = orb_advertise(ORB_ID(vehicle_gps_position), &_report);
|
||||
} else {
|
||||
_report_gps_pos_pub = orb_advertise(ORB_ID(vehicle_gps_position), &_report_gps_pos);
|
||||
}
|
||||
}
|
||||
if (_p_report_sat_info && (helper_ret & 2)) {
|
||||
if (_report_sat_info_pub > 0) {
|
||||
orb_publish(ORB_ID(satellite_info), _report_sat_info_pub, _p_report_sat_info);
|
||||
|
||||
} else {
|
||||
_report_sat_info_pub = orb_advertise(ORB_ID(satellite_info), _p_report_sat_info);
|
||||
}
|
||||
}
|
||||
}
|
||||
|
||||
last_rate_count++;
|
||||
if (helper_ret & 1) { // consider only pos info updates for rate calculation */
|
||||
last_rate_count++;
|
||||
}
|
||||
|
||||
/* measure update rate every 5 seconds */
|
||||
if (hrt_absolute_time() - last_rate_measurement > RATE_MEASUREMENT_PERIOD) {
|
||||
@@ -446,12 +481,13 @@ GPS::print_info()
|
||||
}
|
||||
|
||||
warnx("port: %s, baudrate: %d, status: %s", _port, _baudrate, (_healthy) ? "OK" : "NOT OK");
|
||||
warnx("sat info: %s", (_p_report_sat_info != nullptr) ? "enabled" : "disabled");
|
||||
|
||||
if (_report.timestamp_position != 0) {
|
||||
warnx("position lock: %dD, satellites: %d, last update: %8.4fms ago", (int)_report.fix_type,
|
||||
_report.satellites_visible, (double)(hrt_absolute_time() - _report.timestamp_position) / 1000.0d);
|
||||
warnx("lat: %d, lon: %d, alt: %d", _report.lat, _report.lon, _report.alt);
|
||||
warnx("eph: %.2fm, epv: %.2fm", (double)_report.eph, (double)_report.epv);
|
||||
if (_report_gps_pos.timestamp_position != 0) {
|
||||
warnx("position lock: %dD, satellites: %d, last update: %8.4fms ago", (int)_report_gps_pos.fix_type,
|
||||
_report_gps_pos.satellites_used, (double)(hrt_absolute_time() - _report_gps_pos.timestamp_position) / 1000.0);
|
||||
warnx("lat: %d, lon: %d, alt: %d", _report_gps_pos.lat, _report_gps_pos.lon, _report_gps_pos.alt);
|
||||
warnx("eph: %.2fm, epv: %.2fm", (double)_report_gps_pos.eph, (double)_report_gps_pos.epv);
|
||||
warnx("rate position: \t%6.2f Hz", (double)_Helper->get_position_update_rate());
|
||||
warnx("rate velocity: \t%6.2f Hz", (double)_Helper->get_velocity_update_rate());
|
||||
warnx("rate publication:\t%6.2f Hz", (double)_rate);
|
||||
@@ -469,7 +505,7 @@ namespace gps
|
||||
|
||||
GPS *g_dev;
|
||||
|
||||
void start(const char *uart_path, bool fake_gps);
|
||||
void start(const char *uart_path, bool fake_gps, bool enable_sat_info);
|
||||
void stop();
|
||||
void test();
|
||||
void reset();
|
||||
@@ -479,7 +515,7 @@ void info();
|
||||
* Start the driver.
|
||||
*/
|
||||
void
|
||||
start(const char *uart_path, bool fake_gps)
|
||||
start(const char *uart_path, bool fake_gps, bool enable_sat_info)
|
||||
{
|
||||
int fd;
|
||||
|
||||
@@ -487,7 +523,7 @@ start(const char *uart_path, bool fake_gps)
|
||||
errx(1, "already started");
|
||||
|
||||
/* create the driver */
|
||||
g_dev = new GPS(uart_path, fake_gps);
|
||||
g_dev = new GPS(uart_path, fake_gps, enable_sat_info);
|
||||
|
||||
if (g_dev == nullptr)
|
||||
goto fail;
|
||||
@@ -580,6 +616,7 @@ gps_main(int argc, char *argv[])
|
||||
/* set to default */
|
||||
const char *device_name = GPS_DEFAULT_UART_PORT;
|
||||
bool fake_gps = false;
|
||||
bool enable_sat_info = false;
|
||||
|
||||
/*
|
||||
* Start/load the driver.
|
||||
@@ -601,7 +638,13 @@ gps_main(int argc, char *argv[])
|
||||
fake_gps = true;
|
||||
}
|
||||
|
||||
gps::start(device_name, fake_gps);
|
||||
/* Detect sat info option */
|
||||
for (int i = 2; i < argc; i++) {
|
||||
if (!strcmp(argv[i], "-s"))
|
||||
enable_sat_info = true;
|
||||
}
|
||||
|
||||
gps::start(device_name, fake_gps, enable_sat_info);
|
||||
}
|
||||
|
||||
if (!strcmp(argv[1], "stop"))
|
||||
@@ -626,5 +669,5 @@ gps_main(int argc, char *argv[])
|
||||
gps::info();
|
||||
|
||||
out:
|
||||
errx(1, "unrecognized command, try 'start', 'stop', 'test', 'reset' or 'status' [-d /dev/ttyS0-n][-f]");
|
||||
errx(1, "unrecognized command, try 'start', 'stop', 'test', 'reset' or 'status' [-d /dev/ttyS0-n][-f][-s]");
|
||||
}
|
||||
|
||||
@@ -62,8 +62,8 @@ protected:
|
||||
uint8_t _rate_count_lat_lon;
|
||||
uint8_t _rate_count_vel;
|
||||
|
||||
float _rate_lat_lon;
|
||||
float _rate_vel;
|
||||
float _rate_lat_lon = 0.0f;
|
||||
float _rate_vel = 0.0f;
|
||||
|
||||
uint64_t _interval_rate_start;
|
||||
};
|
||||
|
||||
@@ -263,7 +263,7 @@ MTK::handle_message(gps_mtk_packet_t &packet)
|
||||
_gps_position->epv = _gps_position->eph; // unknown in mtk custom mode, so we cheat with eph
|
||||
_gps_position->vel_m_s = ((float)packet.ground_speed) * 1e-2f; // from cm/s to m/s
|
||||
_gps_position->cog_rad = ((float)packet.heading) * M_DEG_TO_RAD_F * 1e-2f; //from deg *100 to rad
|
||||
_gps_position->satellites_visible = packet.satellites;
|
||||
_gps_position->satellites_used = packet.satellites;
|
||||
|
||||
/* convert time and date information to unix timestamp */
|
||||
struct tm timeinfo; //TODO: test this conversion
|
||||
|
||||
+604
-448
File diff suppressed because it is too large
Load Diff
+394
-279
File diff suppressed because it is too large
Load Diff
@@ -226,7 +226,7 @@ build_gps_response(uint8_t *buffer, size_t *size)
|
||||
msg.sensor_id = GPS_SENSOR_ID;
|
||||
msg.sensor_text_id = GPS_SENSOR_TEXT_ID;
|
||||
|
||||
msg.gps_num_sat = gps.satellites_visible;
|
||||
msg.gps_num_sat = gps.satellites_used;
|
||||
|
||||
/* The GPS fix type: 0 = none, 2 = 2D, 3 = 3D */
|
||||
msg.gps_fix_char = (uint8_t)(gps.fix_type + 48);
|
||||
|
||||
@@ -310,7 +310,7 @@ void TECS::_update_throttle(float throttle_cruise, const math::Matrix<3,3> &rotM
|
||||
STEdot_dem = STEdot_dem + _rollComp * (1.0f / constrain(cosPhi , 0.1f, 1.0f) - 1.0f);
|
||||
|
||||
if (STEdot_dem >= 0) {
|
||||
ff_throttle = nomThr + STEdot_dem / _STEdot_max * (1.0f - nomThr);
|
||||
ff_throttle = nomThr + STEdot_dem / _STEdot_max * (_THRmaxf - nomThr);
|
||||
|
||||
} else {
|
||||
ff_throttle = nomThr - STEdot_dem / _STEdot_min * nomThr;
|
||||
|
||||
@@ -182,7 +182,7 @@ arming_state_transition(struct vehicle_status_s *status, /// current
|
||||
if (status->condition_power_input_valid && (status->avionics_power_rail_voltage > 0.0f) &&
|
||||
(status->avionics_power_rail_voltage < 4.9f)) {
|
||||
|
||||
mavlink_log_critical(mavlink_fd, "#audio: NOT ARMING: Avionics power low: %6.2f V.", status->avionics_power_rail_voltage);
|
||||
mavlink_log_critical(mavlink_fd, "#audio: NOT ARMING: Avionics power low: %6.2f V.", (double)status->avionics_power_rail_voltage);
|
||||
valid_transition = false;
|
||||
}
|
||||
}
|
||||
@@ -638,7 +638,7 @@ int prearm_check(const struct vehicle_status_s *status, const int mavlink_fd)
|
||||
}
|
||||
|
||||
if (!status->is_rotary_wing) {
|
||||
int fd = open(AIRSPEED_DEVICE_PATH, O_RDONLY);
|
||||
fd = open(AIRSPEED_DEVICE_PATH, O_RDONLY);
|
||||
|
||||
if (fd < 0) {
|
||||
mavlink_log_critical(mavlink_fd, "#audio: FAIL: AIRSPEED SENSOR MISSING");
|
||||
|
||||
@@ -677,7 +677,7 @@ protected:
|
||||
cm_uint16_from_m_float(gps.epv),
|
||||
gps.vel_m_s * 100.0f,
|
||||
_wrap_2pi(gps.cog_rad) * M_RAD_TO_DEG_F * 1e2f,
|
||||
gps.satellites_visible);
|
||||
gps.satellites_used);
|
||||
}
|
||||
}
|
||||
};
|
||||
|
||||
@@ -751,9 +751,8 @@ MavlinkReceiver::handle_message_hil_gps(mavlink_message_t *msg)
|
||||
hil_gps.vel_ned_valid = true;
|
||||
hil_gps.cog_rad = _wrap_pi(gps.cog * M_DEG_TO_RAD_F * 1e-2f);
|
||||
|
||||
hil_gps.timestamp_satellites = timestamp;
|
||||
hil_gps.fix_type = gps.fix_type;
|
||||
hil_gps.satellites_visible = gps.satellites_visible;
|
||||
hil_gps.satellites_used = gps.satellites_visible; //TODO: rename mavlink_hil_gps_t sats visible to used?
|
||||
|
||||
if (_gps_pub < 0) {
|
||||
_gps_pub = orb_advertise(ORB_ID(vehicle_gps_position), &hil_gps);
|
||||
|
||||
@@ -915,6 +915,10 @@ int position_estimator_inav_thread_main(int argc, char *argv[])
|
||||
memcpy(x_est_prev, x_est, sizeof(x_est));
|
||||
memcpy(y_est_prev, y_est, sizeof(y_est));
|
||||
}
|
||||
} else {
|
||||
/* gradually reset xy velocity estimates */
|
||||
inertial_filter_correct(-x_est[1], dt, x_est, 1, params.w_xy_res_v);
|
||||
inertial_filter_correct(-y_est[1], dt, y_est, 1, params.w_xy_res_v);
|
||||
}
|
||||
|
||||
/* detect land */
|
||||
@@ -930,6 +934,9 @@ int position_estimator_inav_thread_main(int argc, char *argv[])
|
||||
landed = false;
|
||||
landed_time = 0;
|
||||
}
|
||||
/* reset xy velocity estimates when landed */
|
||||
x_est[1] = 0.0f;
|
||||
y_est[1] = 0.0f;
|
||||
|
||||
} else {
|
||||
if (alt_disp2 < land_disp2 && thrust < params.land_thr) {
|
||||
|
||||
@@ -46,6 +46,7 @@ PARAM_DEFINE_FLOAT(INAV_W_Z_SONAR, 3.0f);
|
||||
PARAM_DEFINE_FLOAT(INAV_W_XY_GPS_P, 1.0f);
|
||||
PARAM_DEFINE_FLOAT(INAV_W_XY_GPS_V, 2.0f);
|
||||
PARAM_DEFINE_FLOAT(INAV_W_XY_FLOW, 5.0f);
|
||||
PARAM_DEFINE_FLOAT(INAV_W_XY_RES_V, 0.5f);
|
||||
PARAM_DEFINE_FLOAT(INAV_W_GPS_FLOW, 0.1f);
|
||||
PARAM_DEFINE_FLOAT(INAV_W_ACC_BIAS, 0.05f);
|
||||
PARAM_DEFINE_FLOAT(INAV_FLOW_K, 0.15f);
|
||||
@@ -65,6 +66,7 @@ int parameters_init(struct position_estimator_inav_param_handles *h)
|
||||
h->w_xy_gps_p = param_find("INAV_W_XY_GPS_P");
|
||||
h->w_xy_gps_v = param_find("INAV_W_XY_GPS_V");
|
||||
h->w_xy_flow = param_find("INAV_W_XY_FLOW");
|
||||
h->w_xy_res_v = param_find("INAV_W_XY_RES_V");
|
||||
h->w_gps_flow = param_find("INAV_W_GPS_FLOW");
|
||||
h->w_acc_bias = param_find("INAV_W_ACC_BIAS");
|
||||
h->flow_k = param_find("INAV_FLOW_K");
|
||||
@@ -87,6 +89,7 @@ int parameters_update(const struct position_estimator_inav_param_handles *h, str
|
||||
param_get(h->w_xy_gps_p, &(p->w_xy_gps_p));
|
||||
param_get(h->w_xy_gps_v, &(p->w_xy_gps_v));
|
||||
param_get(h->w_xy_flow, &(p->w_xy_flow));
|
||||
param_get(h->w_xy_res_v, &(p->w_xy_res_v));
|
||||
param_get(h->w_gps_flow, &(p->w_gps_flow));
|
||||
param_get(h->w_acc_bias, &(p->w_acc_bias));
|
||||
param_get(h->flow_k, &(p->flow_k));
|
||||
|
||||
@@ -47,6 +47,7 @@ struct position_estimator_inav_params {
|
||||
float w_xy_gps_p;
|
||||
float w_xy_gps_v;
|
||||
float w_xy_flow;
|
||||
float w_xy_res_v;
|
||||
float w_gps_flow;
|
||||
float w_acc_bias;
|
||||
float flow_k;
|
||||
@@ -66,6 +67,7 @@ struct position_estimator_inav_param_handles {
|
||||
param_t w_xy_gps_p;
|
||||
param_t w_xy_gps_v;
|
||||
param_t w_xy_flow;
|
||||
param_t w_xy_res_v;
|
||||
param_t w_gps_flow;
|
||||
param_t w_acc_bias;
|
||||
param_t flow_k;
|
||||
|
||||
+31
-19
@@ -74,6 +74,7 @@
|
||||
#include <uORB/topics/vehicle_global_position.h>
|
||||
#include <uORB/topics/position_setpoint_triplet.h>
|
||||
#include <uORB/topics/vehicle_gps_position.h>
|
||||
#include <uORB/topics/satellite_info.h>
|
||||
#include <uORB/topics/vehicle_vicon_position.h>
|
||||
#include <uORB/topics/vehicle_global_velocity_setpoint.h>
|
||||
#include <uORB/topics/optical_flow.h>
|
||||
@@ -141,6 +142,8 @@ PARAM_DEFINE_INT32(SDLOG_EXT, -1);
|
||||
fds[fdsc_count].events = POLLIN; \
|
||||
fdsc_count++;
|
||||
|
||||
#define MIN(X,Y) ((X) < (Y) ? (X) : (Y))
|
||||
|
||||
static bool main_thread_should_exit = false; /**< Deamon exit flag */
|
||||
static bool thread_running = false; /**< Deamon status flag */
|
||||
static int deamon_task; /**< Handle of deamon task / thread */
|
||||
@@ -944,6 +947,7 @@ int sdlog2_thread_main(int argc, char *argv[])
|
||||
struct tecs_status_s tecs_status;
|
||||
struct system_power_s system_power;
|
||||
struct servorail_status_s servorail_status;
|
||||
struct satellite_info_s sat_info;
|
||||
struct wind_estimate_s wind_estimate;
|
||||
} buf;
|
||||
|
||||
@@ -1007,6 +1011,7 @@ int sdlog2_thread_main(int argc, char *argv[])
|
||||
int global_pos_sub;
|
||||
int triplet_sub;
|
||||
int gps_pos_sub;
|
||||
int sat_info_sub;
|
||||
int vicon_pos_sub;
|
||||
int flow_sub;
|
||||
int rc_sub;
|
||||
@@ -1026,6 +1031,7 @@ int sdlog2_thread_main(int argc, char *argv[])
|
||||
subs.cmd_sub = orb_subscribe(ORB_ID(vehicle_command));
|
||||
subs.status_sub = orb_subscribe(ORB_ID(vehicle_status));
|
||||
subs.gps_pos_sub = orb_subscribe(ORB_ID(vehicle_gps_position));
|
||||
subs.sat_info_sub = orb_subscribe(ORB_ID(satellite_info));
|
||||
subs.sensor_sub = orb_subscribe(ORB_ID(sensor_combined));
|
||||
subs.att_sub = orb_subscribe(ORB_ID(vehicle_attitude));
|
||||
subs.att_sp_sub = orb_subscribe(ORB_ID(vehicle_attitude_setpoint));
|
||||
@@ -1066,11 +1072,14 @@ int sdlog2_thread_main(int argc, char *argv[])
|
||||
hrt_abstime barometer_timestamp = 0;
|
||||
hrt_abstime differential_pressure_timestamp = 0;
|
||||
|
||||
/* initialize calculated mean SNR */
|
||||
float snr_mean = 0.0f;
|
||||
|
||||
/* enable logging on start if needed */
|
||||
if (log_on_start) {
|
||||
/* check GPS topic to get GPS time */
|
||||
if (log_name_timestamp) {
|
||||
if (copy_if_updated(ORB_ID(vehicle_gps_position), subs.gps_pos_sub, &buf_gps_pos)) {
|
||||
if (!orb_copy(ORB_ID(vehicle_gps_position), subs.gps_pos_sub, &buf_gps_pos)) {
|
||||
gps_time = buf_gps_pos.time_gps_usec;
|
||||
}
|
||||
}
|
||||
@@ -1128,14 +1137,6 @@ int sdlog2_thread_main(int argc, char *argv[])
|
||||
/* --- GPS POSITION - UNIT #1 --- */
|
||||
if (gps_pos_updated) {
|
||||
|
||||
float snr_mean = 0.0f;
|
||||
|
||||
for (unsigned i = 0; i < buf_gps_pos.satellites_visible; i++) {
|
||||
snr_mean += buf_gps_pos.satellite_snr[i];
|
||||
}
|
||||
|
||||
snr_mean /= buf_gps_pos.satellites_visible;
|
||||
|
||||
log_msg.msg_type = LOG_GPS_MSG;
|
||||
log_msg.body.log_GPS.gps_time = buf_gps_pos.time_gps_usec;
|
||||
log_msg.body.log_GPS.fix_type = buf_gps_pos.fix_type;
|
||||
@@ -1148,44 +1149,55 @@ int sdlog2_thread_main(int argc, char *argv[])
|
||||
log_msg.body.log_GPS.vel_e = buf_gps_pos.vel_e_m_s;
|
||||
log_msg.body.log_GPS.vel_d = buf_gps_pos.vel_d_m_s;
|
||||
log_msg.body.log_GPS.cog = buf_gps_pos.cog_rad;
|
||||
log_msg.body.log_GPS.sats = buf_gps_pos.satellites_visible;
|
||||
log_msg.body.log_GPS.sats = buf_gps_pos.satellites_used;
|
||||
log_msg.body.log_GPS.snr_mean = snr_mean;
|
||||
log_msg.body.log_GPS.noise_per_ms = buf_gps_pos.noise_per_ms;
|
||||
log_msg.body.log_GPS.jamming_indicator = buf_gps_pos.jamming_indicator;
|
||||
LOGBUFFER_WRITE_AND_COUNT(GPS);
|
||||
}
|
||||
|
||||
/* --- SATELLITE INFO - UNIT #1 --- */
|
||||
if (_extended_logging) {
|
||||
|
||||
if (copy_if_updated(ORB_ID(satellite_info), subs.sat_info_sub, &buf.sat_info)) {
|
||||
|
||||
if (_extended_logging) {
|
||||
/* log the SNR of each satellite for a detailed view of signal quality */
|
||||
unsigned gps_msg_max_snr = sizeof(buf_gps_pos.satellite_snr) / sizeof(buf_gps_pos.satellite_snr[0]);
|
||||
unsigned sat_info_count = MIN(buf.sat_info.count, sizeof(buf.sat_info.snr) / sizeof(buf.sat_info.snr[0]));
|
||||
unsigned log_max_snr = sizeof(log_msg.body.log_GS0A.satellite_snr) / sizeof(log_msg.body.log_GS0A.satellite_snr[0]);
|
||||
|
||||
log_msg.msg_type = LOG_GS0A_MSG;
|
||||
memset(&log_msg.body.log_GS0A, 0, sizeof(log_msg.body.log_GS0A));
|
||||
/* fill set A */
|
||||
for (unsigned i = 0; i < gps_msg_max_snr; i++) {
|
||||
snr_mean = 0.0f;
|
||||
|
||||
int satindex = buf_gps_pos.satellite_prn[i] - 1;
|
||||
/* fill set A and calculate mean SNR */
|
||||
for (unsigned i = 0; i < sat_info_count; i++) {
|
||||
|
||||
snr_mean += buf.sat_info.snr[i];
|
||||
|
||||
int satindex = buf.sat_info.svid[i] - 1;
|
||||
|
||||
/* handles index exceeding and wraps to to arithmetic errors */
|
||||
if ((satindex >= 0) && (satindex < (int)log_max_snr)) {
|
||||
/* map satellites by their ID so that logs from two receivers can be compared */
|
||||
log_msg.body.log_GS0A.satellite_snr[satindex] = buf_gps_pos.satellite_snr[i];
|
||||
log_msg.body.log_GS0A.satellite_snr[satindex] = buf.sat_info.snr[i];
|
||||
}
|
||||
}
|
||||
LOGBUFFER_WRITE_AND_COUNT(GS0A);
|
||||
snr_mean /= sat_info_count;
|
||||
|
||||
log_msg.msg_type = LOG_GS0B_MSG;
|
||||
memset(&log_msg.body.log_GS0B, 0, sizeof(log_msg.body.log_GS0B));
|
||||
|
||||
/* fill set B */
|
||||
for (unsigned i = 0; i < gps_msg_max_snr; i++) {
|
||||
for (unsigned i = 0; i < sat_info_count; i++) {
|
||||
|
||||
/* get second bank of satellites, thus deduct bank size from index */
|
||||
int satindex = buf_gps_pos.satellite_prn[i] - 1 - log_max_snr;
|
||||
int satindex = buf.sat_info.svid[i] - 1 - log_max_snr;
|
||||
|
||||
/* handles index exceeding and wraps to to arithmetic errors */
|
||||
if ((satindex >= 0) && (satindex < (int)log_max_snr)) {
|
||||
/* map satellites by their ID so that logs from two receivers can be compared */
|
||||
log_msg.body.log_GS0B.satellite_snr[satindex] = buf_gps_pos.satellite_snr[i];
|
||||
log_msg.body.log_GS0B.satellite_snr[satindex] = buf.sat_info.snr[i];
|
||||
}
|
||||
}
|
||||
LOGBUFFER_WRITE_AND_COUNT(GS0B);
|
||||
|
||||
@@ -86,7 +86,7 @@ PARAM_DEFINE_INT32(CBRK_IO_SAFETY, 0);
|
||||
bool circuit_breaker_enabled(const char* breaker, int32_t magic)
|
||||
{
|
||||
int32_t val;
|
||||
(void)param_get(param_find(breaker), val);
|
||||
(void)param_get(param_find(breaker), &val);
|
||||
|
||||
return (val == magic);
|
||||
}
|
||||
|
||||
@@ -40,6 +40,15 @@
|
||||
#ifndef CIRCUIT_BREAKER_H_
|
||||
#define CIRCUIT_BREAKER_H_
|
||||
|
||||
/* SAFETY WARNING -- SAFETY WARNING -- SAFETY WARNING
|
||||
*
|
||||
* OBEY THE DOCUMENTATION FOR ALL CIRCUIT BREAKERS HERE,
|
||||
* ENSURE TO READ CAREFULLY ALL SAFETY WARNINGS.
|
||||
* http://pixhawk.org/dev/circuit_breakers
|
||||
*
|
||||
* CIRCUIT BREAKERS ARE NOT PART OF THE STANDARD OPERATION PROCEDURE
|
||||
* AND MAY DISABLE CHECKS THAT ARE VITAL FOR SAFE FLIGHT.
|
||||
*/
|
||||
#define CBRK_SUPPLY_CHK_KEY 894281
|
||||
#define CBRK_RATE_CTRL_KEY 140253
|
||||
#define CBRK_IO_SAFETY_KEY 22027
|
||||
|
||||
@@ -40,6 +40,7 @@
|
||||
#include "topics/parameter_update.h"
|
||||
#include "topics/actuator_controls.h"
|
||||
#include "topics/vehicle_gps_position.h"
|
||||
#include "topics/satellite_info.h"
|
||||
#include "topics/sensor_combined.h"
|
||||
#include "topics/vehicle_attitude.h"
|
||||
#include "topics/vehicle_global_position.h"
|
||||
@@ -88,6 +89,7 @@ T Subscription<T>::getData() {
|
||||
template class __EXPORT Subscription<parameter_update_s>;
|
||||
template class __EXPORT Subscription<actuator_controls_s>;
|
||||
template class __EXPORT Subscription<vehicle_gps_position_s>;
|
||||
template class __EXPORT Subscription<satellite_info_s>;
|
||||
template class __EXPORT Subscription<sensor_combined_s>;
|
||||
template class __EXPORT Subscription<vehicle_attitude_s>;
|
||||
template class __EXPORT Subscription<vehicle_global_position_s>;
|
||||
|
||||
@@ -75,6 +75,9 @@ ORB_DEFINE(sensor_combined, struct sensor_combined_s);
|
||||
#include "topics/vehicle_gps_position.h"
|
||||
ORB_DEFINE(vehicle_gps_position, struct vehicle_gps_position_s);
|
||||
|
||||
#include "topics/satellite_info.h"
|
||||
ORB_DEFINE(satellite_info, struct satellite_info_s);
|
||||
|
||||
#include "topics/home_position.h"
|
||||
ORB_DEFINE(home_position, struct home_position_s);
|
||||
|
||||
|
||||
@@ -0,0 +1,89 @@
|
||||
/****************************************************************************
|
||||
*
|
||||
* Copyright (C) 2014 PX4 Development Team. All rights reserved.
|
||||
* Author: @author Thomas Gubler <thomasgubler@student.ethz.ch>
|
||||
* @author Julian Oes <joes@student.ethz.ch>
|
||||
* @author Lorenz Meier <lm@inf.ethz.ch>
|
||||
*
|
||||
* Redistribution and use in source and binary forms, with or without
|
||||
* modification, are permitted provided that the following conditions
|
||||
* are met:
|
||||
*
|
||||
* 1. Redistributions of source code must retain the above copyright
|
||||
* notice, this list of conditions and the following disclaimer.
|
||||
* 2. Redistributions in binary form must reproduce the above copyright
|
||||
* notice, this list of conditions and the following disclaimer in
|
||||
* the documentation and/or other materials provided with the
|
||||
* distribution.
|
||||
* 3. Neither the name PX4 nor the names of its contributors may be
|
||||
* used to endorse or promote products derived from this software
|
||||
* without specific prior written permission.
|
||||
*
|
||||
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
|
||||
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
|
||||
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
|
||||
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
|
||||
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
|
||||
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
|
||||
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
|
||||
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
|
||||
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
|
||||
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
|
||||
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
|
||||
* POSSIBILITY OF SUCH DAMAGE.
|
||||
*
|
||||
****************************************************************************/
|
||||
|
||||
/**
|
||||
* @file satellite_info.h
|
||||
* Definition of the GNSS satellite info uORB topic.
|
||||
*/
|
||||
|
||||
#ifndef TOPIC_SAT_INFO_H_
|
||||
#define TOPIC_SAT_INFO_H_
|
||||
|
||||
#include <stdint.h>
|
||||
#include "../uORB.h"
|
||||
|
||||
/**
|
||||
* @addtogroup topics
|
||||
* @{
|
||||
*/
|
||||
|
||||
/**
|
||||
* GNSS Satellite Info.
|
||||
*/
|
||||
|
||||
#define SAT_INFO_MAX_SATELLITES 20
|
||||
|
||||
struct satellite_info_s {
|
||||
uint64_t timestamp; /**< Timestamp of satellite info */
|
||||
uint8_t count; /**< Number of satellites in satellite info */
|
||||
uint8_t svid[SAT_INFO_MAX_SATELLITES]; /**< Space vehicle ID [1..255], see scheme below */
|
||||
uint8_t used[SAT_INFO_MAX_SATELLITES]; /**< 0: Satellite not used, 1: used for navigation */
|
||||
uint8_t elevation[SAT_INFO_MAX_SATELLITES]; /**< Elevation (0: right on top of receiver, 90: on the horizon) of satellite */
|
||||
uint8_t azimuth[SAT_INFO_MAX_SATELLITES]; /**< Direction of satellite, 0: 0 deg, 255: 360 deg. */
|
||||
uint8_t snr[SAT_INFO_MAX_SATELLITES]; /**< dBHz, Signal to noise ratio of satellite C/N0, range 0..99, zero when not tracking this satellite. */
|
||||
};
|
||||
|
||||
/**
|
||||
* NAV_SVINFO space vehicle ID (svid) scheme according to u-blox protocol specs
|
||||
* u-bloxM8-V15_ReceiverDescriptionProtocolSpec_Public_(UBX-13003221).pdf
|
||||
*
|
||||
* GPS 1-32
|
||||
* SBAS 120-158
|
||||
* Galileo 211-246
|
||||
* BeiDou 159-163, 33-64
|
||||
* QZSS 193-197
|
||||
* GLONASS 65-96, 255
|
||||
*
|
||||
*/
|
||||
|
||||
/**
|
||||
* @}
|
||||
*/
|
||||
|
||||
/* register this as object request broker structure */
|
||||
ORB_DECLARE(satellite_info);
|
||||
|
||||
#endif
|
||||
@@ -82,14 +82,7 @@ struct vehicle_gps_position_s {
|
||||
uint64_t timestamp_time; /**< Timestamp for time information */
|
||||
uint64_t time_gps_usec; /**< Timestamp (microseconds in GPS format), this is the timestamp which comes from the gps module */
|
||||
|
||||
uint64_t timestamp_satellites; /**< Timestamp for sattelite information */
|
||||
uint8_t satellites_visible; /**< Number of satellites visible. If unknown, set to 255 */
|
||||
uint8_t satellite_prn[20]; /**< Global satellite ID */
|
||||
uint8_t satellite_used[20]; /**< 0: Satellite not used, 1: used for localization */
|
||||
uint8_t satellite_elevation[20]; /**< Elevation (0: right on top of receiver, 90: on the horizon) of satellite */
|
||||
uint8_t satellite_azimuth[20]; /**< Direction of satellite, 0: 0 deg, 255: 360 deg. */
|
||||
uint8_t satellite_snr[20]; /**< dBHz, Signal to noise ratio of satellite C/N0, range 0..99, zero when not tracking this satellite. */
|
||||
bool satellite_info_available; /**< 0 for no info, 1 for info available */
|
||||
uint8_t satellites_used; /**< Number of satellites used */
|
||||
};
|
||||
|
||||
/**
|
||||
|
||||
@@ -64,6 +64,7 @@ static void do_show_print(void *arg, param_t param);
|
||||
static void do_set(const char* name, const char* val, bool fail_on_not_found);
|
||||
static void do_compare(const char* name, const char* vals[], unsigned comparisons);
|
||||
static void do_reset(void);
|
||||
static void do_reset_nostart(void);
|
||||
|
||||
int
|
||||
param_main(int argc, char *argv[])
|
||||
@@ -142,6 +143,10 @@ param_main(int argc, char *argv[])
|
||||
if (!strcmp(argv[1], "reset")) {
|
||||
do_reset();
|
||||
}
|
||||
|
||||
if (!strcmp(argv[1], "reset_nostart")) {
|
||||
do_reset_nostart();
|
||||
}
|
||||
}
|
||||
|
||||
errx(1, "expected a command, try 'load', 'import', 'show', 'set', 'compare', 'select' or 'save'");
|
||||
@@ -427,3 +432,26 @@ do_reset(void)
|
||||
exit(0);
|
||||
}
|
||||
}
|
||||
|
||||
static void
|
||||
do_reset_nostart(void)
|
||||
{
|
||||
|
||||
int32_t autostart;
|
||||
int32_t autoconfig;
|
||||
|
||||
(void)param_get(param_find("SYS_AUTOSTART"), &autostart);
|
||||
(void)param_get(param_find("SYS_AUTOCONFIG"), &autoconfig);
|
||||
|
||||
param_reset_all();
|
||||
|
||||
(void)param_set(param_find("SYS_AUTOSTART"), &autostart);
|
||||
(void)param_set(param_find("SYS_AUTOCONFIG"), &autoconfig);
|
||||
|
||||
if (param_save_default()) {
|
||||
warnx("Param export failed.");
|
||||
exit(1);
|
||||
} else {
|
||||
exit(0);
|
||||
}
|
||||
}
|
||||
|
||||
Reference in New Issue
Block a user